Analytical Functions

Analytical solutions for 2D aerofoil based on thin plates theory

Author: Salvatore Maraniello

Date: 23 May 2017

References:

  1. Simpson, R.J.S., Palacios, R. & Murua, J., 2013. Induced-Drag Calculations in the Unsteady Vortex Lattice Method. AIAA Journal, 51(7), pp.1775–1779.

  2. Gulcat, U., 2009. Propulsive Force of a Flexible Flapping Thin Airfoil. Journal of Aircraft, 46(2), pp.465–473.